Method presented by which directional stability derivative Cns, rate of change of yawing moment coefficient with sideslip angle, can be evaluated for conventional airplane from flight records of lateral or directional oscillation.


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    Title :

    Simplified method for determining from flight data rate of change of yawing-moment coefficient with sideslip


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Bishop, R.C. (author) / Lomax, H. (author)


    Publication date :

    1946


    Size :

    8 pages


    Remarks:

    4 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :